The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Nov. 20, 2018

Filed:

Apr. 01, 2014
Applicant:

Airbus Defence and Space Sas, Les Mureaux, FR;

Inventor:

Audrey Menochet, Le Bouscat, FR;

Assignee:

ARIANEGROUP SAS, Paris, FR;

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B29C 65/00 (2006.01); B29C 65/34 (2006.01); B29C 65/48 (2006.01); B29C 65/50 (2006.01); B32B 5/02 (2006.01); B32B 27/08 (2006.01); B32B 27/12 (2006.01); B32B 27/32 (2006.01); C08J 5/12 (2006.01); B29C 65/20 (2006.01); B29C 65/36 (2006.01); B29L 31/30 (2006.01); B29C 65/02 (2006.01); B29C 35/02 (2006.01); B29K 71/00 (2006.01); B29L 7/00 (2006.01); B29L 9/00 (2006.01);
U.S. Cl.
CPC ...
B29C 66/712 (2013.01); B29C 65/20 (2013.01); B29C 65/344 (2013.01); B29C 65/348 (2013.01); B29C 65/364 (2013.01); B29C 65/4815 (2013.01); B29C 65/5021 (2013.01); B29C 65/5028 (2013.01); B29C 65/5057 (2013.01); B29C 66/1122 (2013.01); B29C 66/3034 (2013.01); B29C 66/45 (2013.01); B29C 66/71 (2013.01); B29C 66/721 (2013.01); B29C 66/7212 (2013.01); B29C 66/7392 (2013.01); B29C 66/73755 (2013.01); B29C 66/742 (2013.01); B29C 66/7465 (2013.01); B29C 66/81455 (2013.01); B32B 5/022 (2013.01); B32B 27/08 (2013.01); B32B 27/12 (2013.01); B32B 27/322 (2013.01); C08J 5/12 (2013.01); B29C 35/02 (2013.01); B29C 65/02 (2013.01); B29C 66/02 (2013.01); B29C 66/02245 (2013.01); B29C 66/7294 (2013.01); B29C 66/73751 (2013.01); B29C 66/919 (2013.01); B29C 66/91443 (2013.01); B29C 66/91645 (2013.01); B29C 66/91655 (2013.01); B29C 66/949 (2013.01); B29C 2035/0211 (2013.01); B29K 2071/00 (2013.01); B29K 2995/0005 (2013.01); B29K 2995/0046 (2013.01); B29K 2995/0087 (2013.01); B29L 2007/008 (2013.01); B29L 2009/00 (2013.01); B29L 2031/3097 (2013.01); B32B 2260/021 (2013.01); B32B 2260/046 (2013.01); B32B 2307/304 (2013.01);
Abstract

A method for producing, by welding, a joint between a thermoplastic matrix composite material and an elastomeric material. The elastomeric material is functionalized by incorporating, onto the surface of the elastomer, a nonwoven fabric consisting of fibers of thermoplastic material. The functionalized surface of the elastomeric material is welded to the thermoplastic material of the composite. The functionalization of the elastomeric material is performed during the vulcanization of the raw elastomer. The vulcanization is performed under a sufficient pressure for the nonwoven fabric placed on the surface of the raw elastomer to become incorporated with same, at least at the surface, during the vulcanization process. The welding operation includes interposing a metal fabric coated with thermoplastic material between the surfaces of the elastomer and the composite that are welded to each other, and passing an electric current through same, resulting in the surface melting of the two materials.


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